CN115443398A - 非致命弹丸 - Google Patents

非致命弹丸 Download PDF

Info

Publication number
CN115443398A
CN115443398A CN202080097249.2A CN202080097249A CN115443398A CN 115443398 A CN115443398 A CN 115443398A CN 202080097249 A CN202080097249 A CN 202080097249A CN 115443398 A CN115443398 A CN 115443398A
Authority
CN
China
Prior art keywords
projectile
rear portion
cylinder
petal
lethal
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN202080097249.2A
Other languages
English (en)
Inventor
A·V·涅斯捷连科
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
M H Levchuk
A VNiesijielianke
Original Assignee
M H Levchuk
A VNiesijielianke
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by M H Levchuk, A VNiesijielianke filed Critical M H Levchuk
Publication of CN115443398A publication Critical patent/CN115443398A/zh
Pending legal-status Critical Current

Links

Images

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/02—Stabilising arrangements
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/02—Stabilising arrangements
    • F42B10/26—Stabilising arrangements using spin
    • F42B10/28—Stabilising arrangements using spin induced by gas action
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
    • F42B10/50—Brake flaps, e.g. inflatable
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/34—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect expanding before or on impact, i.e. of dumdum or mushroom type

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)

Abstract

本发明涉及一种非致命弹丸，所述非致命弹丸包括圆柱体(2)形式的后部部分，所述圆柱体(2)联接至至少两个对称瓣状冲击元件(1)，所述至少两个对称瓣状冲击元件(1)能够在离开枪膛时打开并且设计成以闭合配置形成圆柱体，所述圆柱体具有等同于所述圆柱形后部部分的直径的外径并且还具有轴向圆柱形开口，所述轴向圆柱形开口过渡成所述弹丸的所述圆柱形后部部分中的轴向开口。所述瓣状元件具有非对称横截面和内圆锥凹槽，所述内圆锥凹槽的基部设置于所述弹丸的后部部分端部处，其中在所述前部部分中，每个瓣状元件具有单向浮雕。

Description

非致命弹丸
技术领域
本发明涉及用于***和刃具武器的非致命弹丸的弹药的生产。
背景技术
最通常地，震荡创伤子弹的制造商利用了弹丸的圆柱形设计(形状)。此类设计的缺点在于，直接冲击面未改变，直至其直接接触相互作用的对象。弹丸的直径受限于武器枪管的直径。这是为什么在此类弹丸中不可能在使用非致命作用弹药情形下的高初始速度和停止作用相组合，该停止作用是未超出对于对象的健康和生命的威胁作用。此外，存在相关于应用范围的一些限制条件，即在一些情况下，这些限制条件为物理上或情况上不可能遵守的。民用所允许的绝大多数创伤性弹丸具有20米以上的使用限制条件，该距离事实上不是自卫距离。
由于增大接触面积，NASTAR弹丸具有对于气流的高正面阻力，该高正面阻力允许弹头的速度显著地降低，并且相应地将弹丸的能量降低至根据高初始速度下的生理学和医学标准的允许范围。这将应用距离减小至实际距离(至多10米)。
在某些情况下，如果需要，该距离可根据客户的需求而增加至所需距离。
对于配备有NASTAR弹头的滑膛武器的子弹测试以实际结果证明了这点。
另外，一些制造商使用了超过枪管直径的弹壳(球或球状(椭圆形)的形式)，由于对于将弹丸挤压于弹壳(该弹壳具有特定几何尺寸以用于武器的正常运作)中的需求，这将使用材料限制于仅软质材料。软质非致命弹丸材料具有低密度，并且因此具有低重量。因此，这影响了弹丸的速度、能量，以及具有类似弹头的子弹在特定类型的自装填武器中起作用的能力。
NASTAR非致命弹丸可由不同硬度的材料制成，这些材料对于对应武器类型中的使用为可接受的，包括一些类型的自装填武器。
根据US9797696B2、US20150330751A1(美国)专利的具有可预测变形和分段式元件的弹头(用于***)为已知的。它们具有视觉上一定程度类似的元件，但它们在任何和操作原理方面根本上不同于NASTAR弹丸。它们设计成施以最大目标伤害，并且在接触目标时展开。
NASTAR非致命弹丸基于通过分段式冲击元件增加接触接触面积的原理，这些分段式冲击元件在接触目标之前的飞行中展开并且防止穿透目标。不存在这种设计的类似物。
发明内容
非致命性弹丸的目的是阻止攻击对象(攻击者)而不引起重大损害，同时防止与任何生物体(无论人类或动物)的生命不相容的创伤。此类弹丸(弹头)用于自卫或防止威胁公民的公共或人身安全的行动。
弹丸的冲击部分的接触面积应为尽可能大的，以传递涉及阻止行动对象的最大能量，同时防止对于生物体的外部和内部器官的穿透和严重伤害。
NASTAR非致命弹丸(弹丸)根据以分段式冲击元件增加接触面积的原理进行工作，这些分段式冲击元件在接触目标之前的飞行中展开并且防止穿透目标。
NASTAR弹丸表示一种整体设计，该整体设计包括分段式元件(两者或更多者)和基部，该基部为联接这些元件的环状物的形式。
分段式元件在离开枪管之后随即展开，从而使接触面积增加数倍。在飞行中，弹丸通过由积聚于瓣状物上气流作用所形成的旋转进行稳定，该气流以飞行器螺旋桨(飞机等)的形式来执行。在弹丸(环状物)的底部，存在如同降落伞的凹槽(开口)，该凹槽防止了飞行中的部署或倒转。
对于NASTAR弹丸的增加接触面积的气流的高正面阻力允许使弹头的速度显著地降低，并且相应地将弹丸的能量降低至根据高初始速度下的生理学和医学标准的可接受参数。
NASTAR弹丸的材料可为基于橡胶或塑料的复合材料，多种材料可添加至该复合材料以增加或反之减小重量。
附图说明
图1示出了静止(飞行、部署)状态的“NASTAR”弹丸(俯视图)。
图2示出了静止(飞行、部署)状态的“NASTAR”弹丸(仰视图)。
图3示出了静止(飞行、部署)状态的“NASTAR”弹丸(侧视图)，其中分段式接触冲击元件(1)连接至连接环(2)。
图4示出了折叠状态的“NASTAR”弹丸(侧视图)。
图5示出了折叠状态的“NASTAR”弹丸(俯视图)。
图6示出了折叠状态的“NASTAR”弹丸(仰视图)。
本发明适合于工业生产。

Claims (1)

1.一种非致命弹丸“NASTAR”，包括后部部分，所述后部部分以圆柱体的形式制成，所述圆柱体联接到至少两个对称瓣状物，所述至少两个对称瓣状物具有圆扇形形式的横截面，所述圆扇形的外径等同于所述圆柱形后部部分的直径，并且在折叠状态下形成了具有轴向圆弧形盲道开口的圆柱体；其特征在于，所述弹丸的后部部分为具有轴向开口的圆柱体的形式，并且所述瓣状元件具有非对称部段并且在折叠状态下形成了圆柱体并具有内圆锥凹槽，所述内圆锥凹槽的基部设置于所述弹丸的后部部分端部处，其中在前部部分，每个瓣状元件具有单向浮雕。
CN202080097249.2A 2019-12-20 2020-05-27 非致命弹丸 Pending CN115443398A (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
UAA201912077 2019-12-20
UAA201912077 2019-12-20
PCT/UA2020/000057 WO2021126136A1 (ru) 2019-12-20 2020-05-27 Снаряд нелетального действия

Publications (1)

Publication Number Publication Date
CN115443398A true CN115443398A (zh) 2022-12-06

Family

ID=76477740

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202080097249.2A Pending CN115443398A (zh) 2019-12-20 2020-05-27 非致命弹丸

Country Status (4)

Country Link
US (1) US20220412705A1 (zh)
EP (1) EP4080155A4 (zh)
CN (1) CN115443398A (zh)
WO (1) WO2021126136A1 (zh)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3952662A (en) * 1974-05-29 1976-04-27 Greenlees William D Non-lethal projectile for riot control
CN1043387A (zh) * 1988-12-05 1990-06-27 埃斯塔勒国立制造股份有限公司 高性能弹丸
US20030041768A1 (en) * 2001-09-05 2003-03-06 Rastegar Jahangir S. Deployable bullets
US7549376B1 (en) * 2005-07-15 2009-06-23 The United States Of America As Represented By The Secretary Of The Army Non-lethal projectile carrier
CN203249550U (zh) * 2013-05-20 2013-10-23 郭三学 一种具有多弹丸的动能弹
US20150345919A1 (en) * 2015-03-19 2015-12-03 Timothy Thor Leach Articulating high-density less-lethal ballistic projectile
CN205607267U (zh) * 2016-05-12 2016-09-28 中国人民武装警察部队工程大学 一种带尾翼的枪发非致命胶袋弹

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2313656A1 (fr) * 1975-06-03 1976-12-31 Cosson Sa Rene Balle, notamment pour cartouche de chasse
US9354027B2 (en) 2013-10-24 2016-05-31 G2 Research Inc. Fragmenting projectile
DK3137843T3 (da) * 2014-04-30 2019-08-26 G9 Holdings Llc Projektil med forbedret ballistik
US9797696B2 (en) 2014-08-14 2017-10-24 OATH Corporation Conic taper tip fracturing projectiles

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3952662A (en) * 1974-05-29 1976-04-27 Greenlees William D Non-lethal projectile for riot control
CN1043387A (zh) * 1988-12-05 1990-06-27 埃斯塔勒国立制造股份有限公司 高性能弹丸
US20030041768A1 (en) * 2001-09-05 2003-03-06 Rastegar Jahangir S. Deployable bullets
US7549376B1 (en) * 2005-07-15 2009-06-23 The United States Of America As Represented By The Secretary Of The Army Non-lethal projectile carrier
CN203249550U (zh) * 2013-05-20 2013-10-23 郭三学 一种具有多弹丸的动能弹
US20150345919A1 (en) * 2015-03-19 2015-12-03 Timothy Thor Leach Articulating high-density less-lethal ballistic projectile
CN205607267U (zh) * 2016-05-12 2016-09-28 中国人民武装警察部队工程大学 一种带尾翼的枪发非致命胶袋弹

Also Published As

Publication number Publication date
US20220412705A1 (en) 2022-12-29
WO2021126136A1 (ru) 2021-06-24
EP4080155A1 (en) 2022-10-26
EP4080155A4 (en) 2023-12-27

Similar Documents

Publication Publication Date Title
US7231875B2 (en) Deployable bullets having a tranquilizer
US9200878B2 (en) Bullets with lateral damage stopping power
US8127683B2 (en) Weapon and weapon system employing the same
US8122810B2 (en) Rocket propelled barrier defense system
US4664034A (en) Fettered shot
US7987790B1 (en) Ring airfoil glider expendable cartridge and glider launching method
US11009321B2 (en) Less-lethal munitions
US20090114112A1 (en) Special purpose small arms ammunition
US6736070B2 (en) Passive action security systems
RU2410625C2 (ru) Сеть для нелетального обездвиживания биообъектов и устройство для ее дистанционного набрасывания
US20220120542A1 (en) Ballistic delivery method and system for injectable formulations
US9702677B2 (en) Ammunition for providing a multilayer flowering upon impact
US6161482A (en) Multi-disk shell and wad
US3906860A (en) Dual purpose projectile
CN115443398A (zh) 非致命弹丸
CA2490458C (en) Extended range less lethal projectile
US20240044625A1 (en) Disruptive projectiles and method of making the same
US20050116090A1 (en) Non-lethal nose cone design
CN113587742B (zh) 一种具有多重冲击破坏机构的复合型防***能弹
RU2009444C1 (ru) Охотничий патрон стрелкового оружия
US11226185B2 (en) Projectile having adaptive expansion characteristics
RU2610021C1 (ru) Пуля для пневматического несмертельного оружия
RU2239151C1 (ru) Ротирующий осколочный боеприпас
RU2410634C1 (ru) Пуля
RU2262652C2 (ru) Пуля

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination